Protuberance placement mastery: Shock wave control integration with Coanda effect to thrust vectoring on a sonic jet-Reference-Cited by-同舟云学术

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Protuberance placement mastery: Shock wave control integration with Coanda effect to thrust vectoring on a sonic jet

Published:2024-09 Issue: Volume:166 Page:105769
ISSN:0955-7997
Container-title:Engineering Analysis with Boundary Elements
language:en
Short-container-title:Engineering Analysis with Boundary Elements

Author:

Soufivand Mohammad Reza,Hojaji Mohammad^ORCID,Razavi Dehkordi Mohammad Hossein

Publisher

Elsevier BV

Reference34 articles.

1. Rocket propulsion elements john;Sutton,2001

2. Theoretical and numerical analyses of aerodynamic characteristics on shock vector control;Wu;J Aerosp Eng,2020

3. Effect of reacting gas on the fluidic thrust vectoring of an axisymmetric nozzle;Chouicha;Propuls Power Res,2020

4. Numerical simulation of fluidic thrust vectoring in the conical nozzle;Hakim;J Adv Res Fluid Mech Therm Sci,2020

5. Sensitivity analysis of counterflow thrust vector control with a three-dimensional rectangular nozzle;Wu;J Aerosp Eng,2021

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